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Virtual Testing of High Lift Systems

机译:高电梯系统的虚拟测试

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Virtual Testing by means of computer simulations of physical models contains a large potential for the improvement of the verification and certification process of an aircraft's high lift system. Rising system complexity (driven by the need for improved A/C efficiency) on one side and shortened development cycles on the other side lead to the need of an extension of the existing, classical test methods. This is why Airbus High Lift Test Department continuously works since a couple of years on the introduction of Virtual Testing as an additional, equivalent test means besides existing, established physical means of compliance such as Test Rigs (TR) and Real Time Simulators, the so called Functional Integration Benches (FIB). Besides the obvious need for highly representative, reliable and efficient computer models, modelling methods and simulation tools this also requires a corresponding Simulation Data- and Process-Management (SDPM), establishing a completely traceable simulation lifecycle management along the aircraft development. Based on COTS Software (SimManager), the High Lift Test Department has specified and developed the High Lift System Test Portal (HLSVT Portal). This system establishes the link between simulation results and the models that were used for their generation. It also controls the post-processing of simulation results. Furthermore it traces the creation of the used models by capturing model inputs and driving the modelling process. The integration of Virtual Test and its Data- and Process-Management into the overall departmental testing process is assured by an interface to the software that is used in the department for global test planning, coordination and administration, the so called Test Management System. This interface is used for import of the definitions of tests that are to be performed on one side as well as to upload the post-processed simulation results for further system requirement's evaluation in the Test Management System on the other side. By this a complete traceability is established between a system requirement, the data used for its evaluation and the models and processes used to produce this data. The presentation gives an overview of the high lift test department and its activities. It shows the current status of implementation of the HLSVT Portal and gives an outlook on further activities. The presentation focuses on the current realization of efficient conduction of test variations and the corresponding post-processing: The evaluation of simulation results, including flexible, definable key value extraction and plot generation is realized by a combination spreadsheet-like definition of post-processing activities (Excel) and the integration of mathematical software (Matlab) into the HLSVT Portal.
机译:通过计算机模拟的虚拟测试物理模型包含了改进飞机的高升力系统的验证和认证过程的大潜力。系统复杂性上升(通过改善A / C效率的需求驱动)在一侧和缩短开发周期导致现有的经典测试方法的延伸需要。这就是为什么空中客车高升降试验部门的持续作用,因为除了现有的额外,等效的测试装置之外,在将虚拟测试引入虚拟测试之外,还建立了符合试验台(TR)和实时模拟器等,所以称为功能集成长凳(FIB)。除了显而易见的高度代表性,可靠和高效的计算机型号,建模方法和仿真工具还需要相应的模拟数据和过程管理(SDPM),沿着飞机开发建立完全可追溯的模拟生命周期管理。基于COTS软件(SimManager),高电梯测试部门已指定并开发出高升降系统测试门户(HLSVT门户)。该系统建立了模拟结果与其生成的模型之间的链接。它还控制模拟结果的后处理。此外,它通过捕获模型输入并驱动建模过程来追踪使用的模型的创建。通过在全球测试计划,协调和管理部门使用的软件中使用的软件的界面确保了虚拟测试的集成以及整个部门测试过程的整体部门测试过程。该接口用于导入在一侧执行的测试定义,以及上传后处理后的仿真结果,以便进一步的系统要求在另一侧的测试管理系统中的评估。通过这种完整的可追溯性,在系统要求之间建立了完整的可追溯性,用于其评估的数据和用于产生此数据的模型和流程。该演示概述了高电梯测试部门及其活动。它显示了HLSVT门户的当前实施状态,并在进一步活动中展开了展望。介绍侧重于目前实现测试变化的有效传导和相应的后处理:模拟结果的评估,包括柔性,可定义的键值提取和绘图生成是通过后处理活动的综合电子表格定义来实现的(Excel)以及数学软件(MATLAB)集成到HLSVT门户中。

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